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Added airfoil data files

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This commit is contained in:
Nicholas Humfrey 2017-04-10 22:19:23 +01:00
parent 0d05d5966a
commit 6b124a8241
1552 changed files with 103042 additions and 0 deletions
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40
airfoil/data/2032c.dat Normal file
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20-32C AIRFOIL
18. 18.
0.000000 0.000000
0.012500 0.019300
0.025000 0.031700
0.050000 0.051300
0.075000 0.066400
0.100000 0.078000
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0.400000 0.100200
0.500000 0.090500
0.600000 0.077100
0.700000 0.061000
0.800000 0.042800
0.900000 0.022900
0.950000 0.012400
1.000000 0.001600
0.000000 0.000000
0.012500 -0.005000
0.025000 -0.004200
0.050000 -0.001000
0.075000 0.002800
0.100000 0.006800
0.150000 0.014500
0.200000 0.021700
0.250000 0.028200
0.300000 0.033300
0.400000 0.038500
0.500000 0.038600
0.600000 0.035000
0.700000 0.028600
0.800000 0.020200
0.900000 0.010000
0.950000 0.004400
1.000000 -0.001600

42
airfoil/data/a18.dat Normal file
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A18 (original)
1.00000 0.00614
0.95000 0.01817
0.90000 0.02858
0.80000 0.04624
0.70000 0.06056
0.60000 0.07197
0.55000 0.07612
0.50000 0.07975
0.45000 0.08293
0.40000 0.08376
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0.30000 0.08383
0.25000 0.08065
0.20000 0.07601
0.15000 0.07026
0.10000 0.06234
0.07500 0.05660
0.05000 0.04923
0.02500 0.03947
0.01250 0.03239
0.00000 0.01865
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0.05000 0.00075
0.07500 0.00000
0.10000 0.00006
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0.20000 0.00475
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0.30000 0.01038
0.35000 0.01353
0.40000 0.01657
0.45000 0.01780
0.50000 0.01884
0.55000 0.01980
0.60000 0.01998
0.70000 0.01924
0.80000 0.01452
0.90000 0.00813
0.95000 0.00434
1.00000 0.00000

80
airfoil/data/a18sm.dat Normal file
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A18 (smoothed)
1.00000 0.00307
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0.00000 0.00000
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104
airfoil/data/a63a108c.dat Normal file
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NASA/AMES 63A108 MOD C AIRFOIL
50. 50.
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.03 .02539
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.125 .03911
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.55 .03810
.60 .03559
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.70 .02906
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.80 .0209
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.85 .0164
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.90 .0120
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.95 .0086
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.97 .0076
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1. .0070
.0 .0
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.995 -.00029
1. .0

181
airfoil/data/ag03.dat Normal file
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AG03 (flat aft bottom)
1.000000 0.000662
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181
airfoil/data/ag04.dat Normal file
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AG04
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181
airfoil/data/ag08.dat Normal file
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@ -0,0 +1,181 @@
AG08
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181
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181
airfoil/data/ag10.dat Normal file
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@ -0,0 +1,181 @@
AG10
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184
airfoil/data/ag11.dat Normal file
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@ -0,0 +1,184 @@
AG11
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161
airfoil/data/ag12.dat Normal file
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161
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AG13
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161
airfoil/data/ag14.dat Normal file
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AG14
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161
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AG16
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161
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AG17
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161
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AG18
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0.137471 -0.013648
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0.164779 -0.013092
0.178481 -0.012727
0.192208 -0.012313
0.205954 -0.011856
0.219719 -0.011360
0.233501 -0.010831
0.247295 -0.010273
0.261106 -0.009689
0.274928 -0.009085
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0.316477 -0.007203
0.330353 -0.006565
0.344245 -0.005927
0.358149 -0.005291
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0.385997 -0.004040
0.399940 -0.003424
0.413885 -0.002820
0.427821 -0.002231
0.441744 -0.001654
0.455658 -0.001093
0.469565 -0.000554
0.483462 -0.000037
0.497351 0.000457
0.511235 0.000930
0.525118 0.001376
0.538994 0.001797
0.552867 0.002192
0.566736 0.002561
0.580603 0.002900
0.594464 0.003210
0.608322 0.003493
0.622175 0.003746
0.636023 0.003968
0.649865 0.004161
0.663706 0.004324
0.677546 0.004455
0.691384 0.004555
0.705222 0.004625
0.719062 0.004664
0.732905 0.004671
0.746746 0.004648
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0.788285 0.004395
0.802137 0.004252
0.815994 0.004077
0.829851 0.003874
0.843710 0.003643
0.857572 0.003382
0.871434 0.003096
0.885298 0.002784
0.899164 0.002445
0.913029 0.002081
0.926896 0.001693
0.940762 0.001283
0.954631 0.000848
0.968473 0.000388
0.982067 -0.000086
0.994071 -0.000507
1.000007 -0.000700

161
airfoil/data/ag19.dat Normal file
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AG19
0.999992 0.000244
0.994067 0.000848
0.982082 0.002113
0.968544 0.003504
0.954708 0.004914
0.940826 0.006276
0.926943 0.007613
0.913056 0.008933
0.899168 0.010245
0.885282 0.011547
0.871396 0.012840
0.857515 0.014123
0.843633 0.015399
0.829754 0.016658
0.815876 0.017909
0.801995 0.019144
0.788118 0.020364
0.774240 0.021567
0.760358 0.022757
0.746480 0.023934
0.732598 0.025098
0.718714 0.026246
0.704832 0.027382
0.690952 0.028505
0.677070 0.029611
0.663191 0.030702
0.649316 0.031769
0.635436 0.032803
0.621559 0.033813
0.607686 0.034792
0.593811 0.035742
0.579936 0.036661
0.566066 0.037549
0.552198 0.038403
0.538328 0.039225
0.524462 0.040010
0.510601 0.040760
0.496741 0.041474
0.482880 0.042149
0.469025 0.042788
0.455177 0.043387
0.441328 0.043948
0.427484 0.044466
0.413649 0.044946
0.399815 0.045383
0.385986 0.045776
0.372169 0.046125
0.358355 0.046428
0.344545 0.046682
0.330750 0.046887
0.316965 0.047037
0.303185 0.047134
0.289421 0.047171
0.275674 0.047146
0.261933 0.047054
0.248213 0.046888
0.234514 0.046643
0.220830 0.046310
0.207177 0.045881
0.193554 0.045344
0.179962 0.044689
0.166424 0.043904
0.152931 0.042974
0.139504 0.041884
0.126159 0.040617
0.112901 0.039151
0.099774 0.037462
0.086793 0.035521
0.074020 0.033292
0.061500 0.030726
0.049351 0.027778
0.037754 0.024395
0.027090 0.020576
0.018069 0.016536
0.011377 0.012750
0.006933 0.009581
0.004065 0.007011
0.002186 0.004880
0.000960 0.003044
0.000235 0.001406
0.000001 -0.000094
0.000368 -0.001552
0.001471 -0.002908
0.003259 -0.004084
0.005777 -0.005206
0.009368 -0.006368
0.014713 -0.007619
0.022632 -0.008896
0.033028 -0.009988
0.044948 -0.010773
0.057612 -0.011265
0.070626 -0.011515
0.083847 -0.011575
0.097208 -0.011488
0.110664 -0.011286
0.124193 -0.010995
0.137773 -0.010634
0.151402 -0.010216
0.165062 -0.009753
0.178754 -0.009253
0.192471 -0.008724
0.206209 -0.008174
0.219965 -0.007607
0.233740 -0.007028
0.247527 -0.006440
0.261333 -0.005847
0.275149 -0.005250
0.288979 -0.004652
0.302827 -0.004054
0.316687 -0.003459
0.330560 -0.002868
0.344449 -0.002282
0.358351 -0.001705
0.372267 -0.001137
0.386195 -0.000582
0.400136 -0.000039
0.414079 0.000487
0.428014 0.000997
0.441936 0.001488
0.455848 0.001958
0.469754 0.002410
0.483648 0.002838
0.497536 0.003246
0.511417 0.003632
0.525297 0.003999
0.539171 0.004338
0.553041 0.004649
0.566907 0.004932
0.580771 0.005183
0.594629 0.005404
0.608483 0.005597
0.622333 0.005758
0.636177 0.005888
0.650015 0.005989
0.663852 0.006060
0.677688 0.006098
0.691521 0.006104
0.705354 0.006082
0.719189 0.006029
0.733027 0.005945
0.746863 0.005833
0.760702 0.005691
0.774544 0.005518
0.788385 0.005316
0.802230 0.005089
0.816081 0.004833
0.829932 0.004550
0.843784 0.004242
0.857640 0.003908
0.871495 0.003551
0.885353 0.003171
0.899212 0.002768
0.913070 0.002347
0.926931 0.001903
0.940790 0.001439
0.954652 0.000956
0.968488 0.000451
0.982076 -0.000064
0.994074 -0.000511
1.000008 -0.000710

164
airfoil/data/ag24.dat Normal file
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@ -0,0 +1,164 @@
AG24 Bubble Dancer DLG by Mark Drela
1.000000 0.000312
0.994048 0.001043
0.982038 0.002630
0.968488 0.004486
0.954647 0.006421
0.940769 0.008378
0.926890 0.010328
0.913006 0.012258
0.899118 0.014165
0.885230 0.016048
0.871339 0.017908
0.857451 0.019744
0.843559 0.021562
0.829670 0.023357
0.815779 0.025130
0.801883 0.026879
0.787989 0.028602
0.774091 0.030297
0.760188 0.031964
0.746285 0.033600
0.732376 0.035204
0.718461 0.036776
0.704547 0.038313
0.690631 0.039813
0.676709 0.041277
0.662788 0.042702
0.648868 0.044087
0.634943 0.045432
0.621017 0.046736
0.607093 0.047997
0.593166 0.049214
0.579236 0.050389
0.565310 0.051517
0.551385 0.052600
0.537456 0.053635
0.523528 0.054622
0.509606 0.055558
0.495682 0.056443
0.481756 0.057276
0.467835 0.058053
0.453918 0.058774
0.440000 0.059437
0.426087 0.060040
0.412180 0.060579
0.398274 0.061053
0.384372 0.061458
0.370481 0.061792
0.356594 0.062050
0.342711 0.062231
0.328841 0.062328
0.314984 0.062338
0.301131 0.062254
0.287296 0.062074
0.273479 0.061789
0.259672 0.061394
0.245889 0.060883
0.232132 0.060248
0.218395 0.059480
0.204696 0.058572
0.191034 0.057514
0.177412 0.056295
0.163854 0.054904
0.150354 0.053325
0.136934 0.051545
0.123613 0.049542
0.110400 0.047296
0.097342 0.044784
0.084457 0.041971
0.071816 0.038832
0.059466 0.035323
0.047533 0.031413
0.036200 0.027083
0.025838 0.022393
0.017129 0.017634
0.010712 0.013341
0.006482 0.009857
0.003763 0.007107
0.001997 0.004865
0.000855 0.002963
0.000198 0.001287
0.000001 -0.000230
0.000293 -0.001719
0.001184 -0.003235
0.002714 -0.004738
0.004994 -0.006301
0.008364 -0.008034
0.013488 -0.010053
0.021193 -0.012377
0.031412 -0.014726
0.043212 -0.016796
0.055804 -0.018519
0.068780 -0.019918
0.081987 -0.021042
0.095351 -0.021938
0.108824 -0.022639
0.122377 -0.023175
0.135989 -0.023565
0.149652 -0.023827
0.163351 -0.023977
0.177085 -0.024026
0.190844 -0.023986
0.204622 -0.023867
0.218421 -0.023675
0.232237 -0.023420
0.246064 -0.023106
0.259909 -0.022740
0.273764 -0.022326
0.287631 -0.021871
0.301514 -0.021381
0.315408 -0.020856
0.329313 -0.020301
0.343234 -0.019718
0.357166 -0.019111
0.371111 -0.018482
0.385067 -0.017835
0.399034 -0.017173
0.413004 -0.016498
0.426962 -0.015813
0.440907 -0.015121
0.454842 -0.014424
0.468769 -0.013723
0.482685 -0.013021
0.496593 -0.012319
0.510494 -0.011617
0.524394 -0.010919
0.538286 -0.010224
0.552174 -0.009535
0.566059 -0.008852
0.579942 -0.008177
0.593817 -0.007511
0.607689 -0.006857
0.621556 -0.006214
0.635419 -0.005585
0.649276 -0.004971
0.663131 -0.004372
0.676986 -0.003788
0.690839 -0.003221
0.704693 -0.002670
0.718548 -0.002136
0.732407 -0.001619
0.746265 -0.001122
0.760127 -0.000645
0.773993 -0.000194
0.787859 0.000230
0.801731 0.000622
0.815611 0.000975
0.829491 0.001286
0.843374 0.001550
0.857263 0.001759
0.871153 0.001909
0.885046 0.001991
0.898943 0.001997
0.912839 0.001920
0.926737 0.001758
0.940634 0.001501
0.954532 0.001149
0.968401 0.000707
0.982019 0.000185
0.994039 -0.000364
1.000000 -0.000659
The AG2x airfoils are intended to be used on composite versions of the
Bubble Dancer and the Allegro-Lite.

164
airfoil/data/ag25.dat Normal file
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@ -0,0 +1,164 @@
AG25 Bubble Dancer DLG by Mark Drela
1.000000 0.000283
0.994054 0.001020
0.982050 0.002599
0.968503 0.004411
0.954662 0.006281
0.940783 0.008151
0.926901 0.010007
0.913016 0.011840
0.899128 0.013652
0.885240 0.015440
0.871350 0.017206
0.857464 0.018949
0.843575 0.020673
0.829689 0.022375
0.815801 0.024054
0.801909 0.025710
0.788021 0.027341
0.774128 0.028945
0.760232 0.030524
0.746336 0.032074
0.732435 0.033595
0.718530 0.035088
0.704627 0.036550
0.690721 0.037981
0.676812 0.039379
0.662904 0.040743
0.648998 0.042070
0.635087 0.043359
0.621176 0.044609
0.607268 0.045818
0.593358 0.046987
0.579446 0.048114
0.565539 0.049198
0.551631 0.050238
0.537721 0.051233
0.523813 0.052182
0.509910 0.053082
0.496007 0.053933
0.482101 0.054735
0.468201 0.055484
0.454307 0.056180
0.440410 0.056821
0.426520 0.057405
0.412636 0.057929
0.398752 0.058392
0.384874 0.058791
0.371005 0.059123
0.357141 0.059386
0.343282 0.059577
0.329435 0.059690
0.315600 0.059723
0.301770 0.059669
0.287958 0.059528
0.274163 0.059290
0.260376 0.058951
0.246613 0.058504
0.232873 0.057942
0.219153 0.057257
0.205468 0.056441
0.191818 0.055484
0.178207 0.054374
0.164654 0.053101
0.151157 0.051646
0.137735 0.049999
0.124408 0.048138
0.111182 0.046040
0.098104 0.043683
0.085190 0.041032
0.072510 0.038059
0.060109 0.034720
0.048112 0.030979
0.036699 0.026809
0.026246 0.022257
0.017438 0.017599
0.010935 0.013364
0.006635 0.009902
0.003867 0.007154
0.002062 0.004904
0.000891 0.002993
0.000210 0.001313
0.000000 -0.000205
0.000317 -0.001680
0.001267 -0.003128
0.002864 -0.004509
0.005203 -0.005914
0.008626 -0.007447
0.013801 -0.009205
0.021556 -0.011179
0.031817 -0.013115
0.043646 -0.014757
0.056256 -0.016068
0.069243 -0.017079
0.082454 -0.017840
0.095819 -0.018399
0.109288 -0.018791
0.122835 -0.019045
0.136441 -0.019178
0.150097 -0.019207
0.163786 -0.019145
0.177511 -0.018999
0.191260 -0.018780
0.205028 -0.018498
0.218817 -0.018158
0.232623 -0.017766
0.246439 -0.017328
0.260273 -0.016850
0.274118 -0.016335
0.287975 -0.015791
0.301848 -0.015223
0.315733 -0.014632
0.329629 -0.014022
0.343541 -0.013395
0.357465 -0.012756
0.371401 -0.012106
0.385350 -0.011449
0.399308 -0.010787
0.413271 -0.010122
0.427222 -0.009457
0.441160 -0.008795
0.455088 -0.008136
0.469010 -0.007485
0.482920 -0.006843
0.496821 -0.006211
0.510717 -0.005588
0.524612 -0.004979
0.538500 -0.004384
0.552383 -0.003803
0.566262 -0.003237
0.580141 -0.002690
0.594011 -0.002160
0.607879 -0.001650
0.621742 -0.001160
0.635601 -0.000692
0.649453 -0.000246
0.663305 0.000177
0.677155 0.000576
0.691004 0.000952
0.704853 0.001303
0.718703 0.001631
0.732557 0.001934
0.746411 0.002212
0.760268 0.002464
0.774128 0.002684
0.787988 0.002875
0.801855 0.003031
0.815728 0.003149
0.829601 0.003225
0.843477 0.003258
0.857358 0.003240
0.871239 0.003171
0.885123 0.003045
0.899010 0.002855
0.912897 0.002596
0.926785 0.002269
0.940673 0.001866
0.954562 0.001387
0.968423 0.000836
0.982034 0.000226
0.994050 -0.000374
1.000000 -0.000680
The AG2x airfoils are intended to be used on composite versions of the
Bubble Dancer and the Allegro-Lite.

164
airfoil/data/ag26.dat Normal file
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@ -0,0 +1,164 @@
AG26 Bubble Dancer DLG by Mark Drela
1.000000 0.000283
0.994061 0.000999
0.982066 0.002505
0.968526 0.004228
0.954693 0.006008
0.940816 0.007759
0.926936 0.009469
0.913054 0.011174
0.899169 0.012856
0.885285 0.014530
0.871402 0.016190
0.857523 0.017832
0.843640 0.019461
0.829761 0.021064
0.815882 0.022652
0.801998 0.024219
0.788119 0.025763
0.774238 0.027291
0.760352 0.028789
0.746468 0.030268
0.732578 0.031719
0.718685 0.033151
0.704794 0.034552
0.690902 0.035926
0.677007 0.037275
0.663114 0.038591
0.649222 0.039874
0.635327 0.041126
0.621434 0.042343
0.607542 0.043523
0.593649 0.044668
0.579754 0.045771
0.565865 0.046837
0.551976 0.047861
0.538085 0.048847
0.524196 0.049789
0.510314 0.050690
0.496430 0.051538
0.482545 0.052336
0.468664 0.053082
0.454789 0.053772
0.440913 0.054407
0.427041 0.054983
0.413176 0.055498
0.399313 0.055953
0.385454 0.056345
0.371607 0.056669
0.357762 0.056927
0.343921 0.057113
0.330095 0.057226
0.316280 0.057262
0.302471 0.057219
0.288679 0.057095
0.274904 0.056884
0.261136 0.056581
0.247392 0.056182
0.233671 0.055680
0.219967 0.055067
0.206299 0.054334
0.192663 0.053472
0.179063 0.052469
0.165520 0.051314
0.152029 0.049989
0.138611 0.048479
0.125281 0.046761
0.112050 0.044812
0.098958 0.042616
0.086022 0.040147
0.073305 0.037380
0.060851 0.034267
0.048780 0.030758
0.037275 0.026799
0.026717 0.022411
0.017800 0.017854
0.011195 0.013657
0.006815 0.010190
0.003988 0.007407
0.002136 0.005117
0.000931 0.003155
0.000227 0.001419
0.000002 -0.000157
0.000342 -0.001683
0.001369 -0.003136
0.003059 -0.004457
0.005487 -0.005761
0.008992 -0.007149
0.014252 -0.008701
0.022090 -0.010375
0.032419 -0.011934
0.044295 -0.013185
0.056934 -0.014106
0.069936 -0.014742
0.083154 -0.015148
0.096518 -0.015373
0.109982 -0.015460
0.123522 -0.015438
0.137115 -0.015327
0.150759 -0.015139
0.164436 -0.014883
0.178145 -0.014564
0.191880 -0.014188
0.205634 -0.013764
0.219407 -0.013295
0.233197 -0.012787
0.247000 -0.012246
0.260819 -0.011674
0.274650 -0.011077
0.288493 -0.010462
0.302352 -0.009830
0.316224 -0.009187
0.330108 -0.008536
0.344007 -0.007882
0.357919 -0.007225
0.371844 -0.006569
0.385781 -0.005919
0.399730 -0.005270
0.413682 -0.004629
0.427624 -0.004000
0.441553 -0.003380
0.455472 -0.002772
0.469385 -0.002184
0.483287 -0.001615
0.497181 -0.001064
0.511069 -0.000532
0.524956 -0.000023
0.538837 0.000463
0.552713 0.000926
0.566586 0.001366
0.580457 0.001780
0.594321 0.002166
0.608182 0.002528
0.622038 0.002860
0.635889 0.003166
0.649734 0.003442
0.663579 0.003691
0.677422 0.003909
0.691263 0.004098
0.705104 0.004259
0.718947 0.004390
0.732793 0.004493
0.746637 0.004565
0.760486 0.004608
0.774336 0.004619
0.788187 0.004597
0.802043 0.004544
0.815905 0.004455
0.829767 0.004330
0.843631 0.004169
0.857499 0.003966
0.871368 0.003725
0.885239 0.003440
0.899112 0.003111
0.912984 0.002735
0.926859 0.002311
0.940732 0.001837
0.954608 0.001313
0.968456 0.000739
0.982055 0.000127
0.994062 -0.000442
1.000000 -0.000716
The AG2x airfoils are intended to be used on composite versions of the
Bubble Dancer and the Allegro-Lite.

165
airfoil/data/ag27.dat Normal file
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@ -0,0 +1,165 @@
AG27 Bubble Dancer DLG by Mark Drela
1.000000 0.000283
0.994180 0.000967
0.982337 0.002388
0.968812 0.004026
0.955011 0.005695
0.941189 0.007338
0.927350 0.008957
0.913497 0.010556
0.899632 0.012140
0.885755 0.013711
0.871872 0.015274
0.857989 0.016826
0.844111 0.018368
0.830237 0.019895
0.816368 0.021406
0.802503 0.022898
0.788640 0.024370
0.774777 0.025821
0.760916 0.027248
0.747055 0.028652
0.733192 0.030032
0.719329 0.031386
0.705466 0.032715
0.691601 0.034018
0.677736 0.035294
0.663871 0.036542
0.650005 0.037761
0.636140 0.038952
0.622275 0.040111
0.608411 0.041238
0.594548 0.042333
0.580687 0.043392
0.566827 0.044415
0.552967 0.045401
0.539110 0.046347
0.525254 0.047252
0.511400 0.048115
0.497547 0.048934
0.483698 0.049707
0.469849 0.050432
0.456003 0.051109
0.442161 0.051733
0.428321 0.052305
0.414484 0.052821
0.400651 0.053281
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0.345368 0.054502
0.331562 0.054641
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0.235251 0.053368
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0.180677 0.050427
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0.100419 0.041546
0.087469 0.039332
0.074753 0.036830
0.062354 0.033994
0.050378 0.030783
0.039021 0.027161
0.028597 0.023137
0.019601 0.018856
0.012624 0.014716
0.007802 0.011144
0.004640 0.008212
0.002567 0.005804
0.001215 0.003765
0.000386 0.001982
0.000020 0.000381
0.000157 -0.001116
0.000954 -0.002587
0.002432 -0.003886
0.004578 -0.005075
0.007597 -0.006275
0.012003 -0.007561
0.018644 -0.008938
0.028138 -0.010257
0.039834 -0.011302
0.052555 -0.011999
0.065723 -0.012396
0.079132 -0.012562
0.092688 -0.012550
0.106349 -0.012399
0.120081 -0.012141
0.133859 -0.011795
0.147675 -0.011377
0.161512 -0.010899
0.175373 -0.010368
0.189252 -0.009794
0.203145 -0.009183
0.217055 -0.008541
0.230978 -0.007875
0.244912 -0.007189
0.258861 -0.006488
0.272820 -0.005778
0.286786 -0.005062
0.300754 -0.004344
0.314716 -0.003631
0.328675 -0.002926
0.342626 -0.002229
0.356566 -0.001545
0.370505 -0.000878
0.384445 -0.000225
0.398379 0.000411
0.412307 0.001027
0.426235 0.001622
0.440162 0.002196
0.454076 0.002747
0.467978 0.003267
0.481879 0.003754
0.495783 0.004209
0.509687 0.004633
0.523590 0.005023
0.537494 0.005381
0.551400 0.005706
0.565305 0.005999
0.579210 0.006258
0.593117 0.006484
0.607024 0.006678
0.620930 0.006839
0.634836 0.006965
0.648742 0.007058
0.662647 0.007118
0.676552 0.007143
0.690457 0.007134
0.704362 0.007090
0.718266 0.007013
0.732172 0.006901
0.746080 0.006756
0.759988 0.006578
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0.787814 0.006127
0.801731 0.005858
0.815650 0.005559
0.829572 0.005234
0.843496 0.004883
0.857422 0.004507
0.871349 0.004106
0.885276 0.003682
0.899202 0.003235
0.913125 0.002764
0.927043 0.002268
0.940954 0.001745
0.954854 0.001194
0.968713 0.000612
0.982285 0.000012
0.994170 -0.000515
1.000000 -0.000752
The AG2x airfoils are intended to be used on composite versions of the
Bubble Dancer and the Allegro-Lite.

181
airfoil/data/ag35.dat Normal file
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@ -0,0 +1,181 @@
AG35
0.999998 0.002490
0.994759 0.003346
0.985091 0.004927
0.973580 0.006810
0.961032 0.008862
0.948054 0.010984
0.934900 0.013135
0.921611 0.015308
0.908313 0.017483
0.895069 0.019649
0.882085 0.021772
0.869641 0.023807
0.857457 0.025799
0.845280 0.027791
0.832888 0.029817
0.820358 0.031820
0.807162 0.033810
0.793920 0.035807
0.780706 0.037799
0.767485 0.039793
0.754283 0.041784
0.741095 0.043773
0.727945 0.045756
0.714849 0.047731
0.701910 0.049683
0.689256 0.051591
0.677196 0.053410
0.665868 0.055118
0.653950 0.056821
0.641439 0.058395
0.629634 0.059724
0.616637 0.061083
0.603508 0.062456
0.590173 0.063850
0.576733 0.065256
0.563295 0.066661
0.549886 0.068063
0.536505 0.069462
0.523180 0.070855
0.509878 0.072246
0.496652 0.073629
0.483548 0.074999
0.470786 0.076333
0.458362 0.077628
0.445896 0.078818
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0.420874 0.081007
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0.395609 0.082920
0.382821 0.083766
0.369887 0.084535
0.356838 0.085222
0.343751 0.085813
0.330663 0.086309
0.317616 0.086705
0.304632 0.086997
0.291702 0.087187
0.278827 0.087271
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0.240294 0.086871
0.227478 0.086509
0.214700 0.086025
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0.009198 0.041532
0.006803 0.039456
0.004900 0.037586
0.003379 0.035865
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0.001229 0.032717
0.000559 0.031249
0.000149 0.029826
0.000002 0.028464
0.000102 0.027126
0.000484 0.025764
0.001210 0.024382
0.002270 0.023013
0.003661 0.021703
0.005428 0.020443
0.007602 0.019219
0.010243 0.018007
0.013475 0.016774
0.017495 0.015493
0.022573 0.014138
0.029012 0.012694
0.037035 0.011190
0.046580 0.009697
0.057315 0.008300
0.068834 0.007045
0.080828 0.005944
0.093116 0.004984
0.105597 0.004152
0.118206 0.003432
0.130910 0.002812
0.143690 0.002279
0.156527 0.001823
0.169413 0.001438
0.182341 0.001114
0.195310 0.000845
0.208312 0.000624
0.221345 0.000445
0.234403 0.000300
0.247480 0.000191
0.260580 0.000110
0.273702 0.000054
0.286843 0.000019
0.300001 0.000000
0.313176 -0.000004
0.326377 -0.000003
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0.352803 -0.000003
0.366016 -0.000002
0.379236 -0.000003
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0.683326 -0.000002
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0.709772 -0.000002
0.722997 -0.000001
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0.749434 -0.000001
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0.775884 -0.000001
0.789107 -0.000001
0.802326 -0.000002
0.815538 -0.000001
0.828754 -0.000002
0.841973 -0.000001
0.855190 0.000000
0.868400 -0.000001
0.881610 0.000000
0.894825 -0.000001
0.908046 -0.000001
0.921267 -0.000001
0.934476 -0.000001
0.947640 -0.000001
0.960660 -0.000001
0.973282 0.000000
0.984898 0.000000
0.994724 -0.000001
1.000001 0.000000

181
airfoil/data/ag36.dat Normal file
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@ -0,0 +1,181 @@
AG36
1.000003 0.002671
0.993991 0.003641
0.983912 0.005266
0.972030 0.007181
0.959208 0.009247
0.946050 0.011369
0.932962 0.013479
0.920159 0.015543
0.907668 0.017556
0.895474 0.019522
0.883699 0.021360
0.870771 0.023227
0.857975 0.025012
0.845188 0.026795
0.832275 0.028596
0.819232 0.030415
0.806149 0.032241
0.793050 0.034067
0.779976 0.035891
0.766906 0.037713
0.753833 0.039537
0.740771 0.041359
0.727741 0.043176
0.714758 0.044986
0.701919 0.046776
0.689366 0.048527
0.677377 0.050200
0.664649 0.051879
0.652447 0.053315
0.640918 0.054568
0.628145 0.055906
0.615243 0.057187
0.602241 0.058477
0.589040 0.059787
0.575726 0.061108
0.562405 0.062429
0.549108 0.063749
0.535834 0.065066
0.522613 0.066377
0.509419 0.067687
0.496304 0.068989
0.483304 0.070278
0.470656 0.071534
0.458359 0.072753
0.445894 0.073861
0.433427 0.074908
0.420872 0.075896
0.408284 0.076816
0.395608 0.077673
0.382819 0.078458
0.369887 0.079171
0.356838 0.079807
0.343750 0.080355
0.330663 0.080811
0.317617 0.081175
0.304632 0.081461
0.291705 0.081662
0.278830 0.081769
0.265979 0.081778
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0.240295 0.081478
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0.105313 0.070415
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0.973288 0.000000
0.984906 0.000000
0.994731 0.000000
1.000000 0.000001

181
airfoil/data/ag37.dat Normal file
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@ -0,0 +1,181 @@
AG37
1.000000 0.003508
0.993634 0.004540
0.983839 0.006128
0.972384 0.007984
0.960126 0.009970
0.947509 0.012015
0.934838 0.014069
0.922272 0.016105
0.909672 0.018147
0.897163 0.020174
0.884502 0.022136
0.872236 0.023744
0.859132 0.025363
0.845998 0.026986
0.832762 0.028622
0.819330 0.030281
0.805796 0.031954
0.792287 0.033623
0.778764 0.035294
0.765277 0.036961
0.751736 0.038634
0.738244 0.040301
0.724795 0.041963
0.711419 0.043616
0.698229 0.045246
0.685362 0.046836
0.672702 0.048400
0.659989 0.049874
0.648296 0.051133
0.636014 0.052350
0.622979 0.053568
0.610109 0.054732
0.597124 0.055906
0.583924 0.057099
0.570608 0.058304
0.557288 0.059508
0.543987 0.060711
0.530692 0.061913
0.517439 0.063111
0.504203 0.064308
0.491039 0.065499
0.478020 0.066675
0.465306 0.067826
0.453088 0.068931
0.440823 0.069934
0.428638 0.070879
0.416395 0.071774
0.404233 0.072598
0.392113 0.073355
0.379952 0.074055
0.367557 0.074706
0.354881 0.075304
0.342042 0.075842
0.329120 0.076312
0.316188 0.076710
0.303310 0.077030
0.290456 0.077269
0.277633 0.077424
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0.251944 0.077457
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0.122032 0.069519
0.109366 0.067704
0.096850 0.065646
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0.074326 0.061155
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@ -0,0 +1,62 @@
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36
airfoil/data/ah7476.dat Normal file
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@ -0,0 +1,36 @@
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102
airfoil/data/ah79100a.dat Normal file
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102
airfoil/data/ah79100b.dat Normal file
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@ -0,0 +1,102 @@
AH 79-100 B AIRFOIL
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102
airfoil/data/ah79100c.dat Normal file
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@ -0,0 +1,102 @@
AH 79-100 C AIRFOIL
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airfoil/data/ah82150f.dat Normal file
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airfoil/data/ah83150q.dat Normal file
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airfoil/data/ah83159.dat Normal file
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airfoil/data/ah85l120.dat Normal file
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AH 85-L-120/17
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airfoil/data/ah88k130.dat Normal file
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AH 88-K-136/16
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121
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AH 93-156
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121
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AH 93-157
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121
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AH 93-K-130/15
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121
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AH 93-K-131/15
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121
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AH 93-K-132/15
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98
airfoil/data/ah93w145.dat Normal file
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@ -0,0 +1,98 @@
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98
airfoil/data/ah93w174.dat Normal file
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@ -0,0 +1,98 @@
AH 93-W-174
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98
airfoil/data/ah93w215.dat Normal file
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@ -0,0 +1,98 @@
AH 93-W-215
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98
airfoil/data/ah93w257.dat Normal file
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@ -0,0 +1,98 @@
AH 93-W-257
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98
airfoil/data/ah93w300.dat Normal file
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@ -0,0 +1,98 @@
AH 93-W-300
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114
airfoil/data/ah93w480b.dat Normal file
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@ -0,0 +1,114 @@
AH 93-W-480B
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121
airfoil/data/ah94145.dat Normal file
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@ -0,0 +1,121 @@
AH 94-145
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121
airfoil/data/ah94156.dat Normal file
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@ -0,0 +1,121 @@
AH 94-156
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98
airfoil/data/ah94w301.dat Normal file
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@ -0,0 +1,98 @@
AH 94-W-301
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121
airfoil/data/ah95160.dat Normal file
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@ -0,0 +1,121 @@
AH 95-160
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86
airfoil/data/ames01.dat Normal file
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@ -0,0 +1,86 @@
NASA/AMES A-01 AIRFOIL
41. 41.
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104
airfoil/data/ames02.dat Normal file
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@ -0,0 +1,104 @@
NASA/AMES A-02 AIRFOIL
50. 50.
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104
airfoil/data/ames03.dat Normal file
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@ -0,0 +1,104 @@
NASA/AMES A-03 AIRFOIL
50. 50.
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80
airfoil/data/amsoil1.dat Normal file
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@ -0,0 +1,80 @@
RUTAN CANARD AIRFOIL
38. 38.
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80
airfoil/data/amsoil2.dat Normal file
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@ -0,0 +1,80 @@
RUTAN WING AIRFOIL
38. 38.
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36
airfoil/data/apex16.dat Normal file
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@ -0,0 +1,36 @@
Apex 16 (normalized using XFOIL date021206)
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0.808974 -0.007347
0.878560 -0.002242
0.946534 -0.000630
1.000000 -0.000093

70
airfoil/data/aquilasm.dat Normal file
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@ -0,0 +1,70 @@
AQUILA 9.3% smoothed
1.00000 0.0
0.99667 0.00057
0.99333 0.00114
0.99000 0.00171
0.98667 0.00228
0.98000 0.00340
0.92667 0.01240
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0.60000 0.06530
0.54667 0.07214
0.49333 0.07799
0.44000 0.08263
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0.34667 0.08710
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0.06000 0.04786
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0.03333 0.03454
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0.02000 0.02587
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0.01000 0.01739
0.00667 0.01377
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0.0 0.0
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0.99333 -0.00006
0.99667 -0.00003
1.00000 0.0

56
airfoil/data/arad10.dat Normal file
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@ -0,0 +1,56 @@
ARA-D 10% AIRFOIL
26. 26.
0.00000 0.00000
.00300 .013713
.01000 .025227
.02000 .035554
.04000 .049237
.07000 .062305
.10000 .070856
.15000 .079585
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.25000 .087500
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.45000 .085232
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.55000 .077289
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.95000 .017146
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1.00000 .007500
0.00000 0.00000
.00300 -.007388
.01000 -.012555
.02000 -.016369
.04000 -.020033
.07000 -.021626
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.15000 -.018291
.20000 -.015159
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.70000 -.006399
.75000 -.006673
.80000 -.006965
.85000 -.007181
.90000 -.007282
.95000 -.007282
.97500 -.007338
1.00000 -.007500

56
airfoil/data/arad13.dat Normal file
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ARA-D 13% AIRFOIL
26. 26.
0.00000 0.00000
.00300 .016690
.01000 .030501
.02000 .042765
.04000 .058860
.07000 .074042
.10000 .083817
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1.00000 .009000
0.00000 0.00000
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.07000 -.030339
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.85000 -.014930
.90000 -.012895
.95000 -.010755
.97500 -.009791
1.00000 -.009000

56
airfoil/data/arad20.dat Normal file
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@ -0,0 +1,56 @@
ARA-D 20% AIRFOIL
26. 26.
0.00000 0.00000
.00300 .022030
.01000 .040200
.02000 .056441
.04000 .078139
.07000 .099311
.10000 .113559
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.75000 .059178
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1.00000 .012500
0.00000 0.00000
.00300 -.010575
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.95000 -.014762
.97500 -.013306
1.00000 -.012500

56
airfoil/data/arad6.dat Normal file
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@ -0,0 +1,56 @@
ARA-D 6% AIRFOIL
26. 26.
0.00000 0.00000
.00300 .009099
.01000 .017152
.02000 .024678
.04000 .035135
.07000 .045809
.10000 .053377
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1.00000 .005500
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.97500 -.003184
1.00000 -.005500

83
airfoil/data/as5045.dat Normal file
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@ -0,0 +1,83 @@
AS5045 (15%)
1.0000 .00125
.99810 .00168
.99262 .00289
.98385 .00461
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.96671 .00018
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1.0000 -.00125
http://amber.aae.uiuc.edu/~ashok/kr2/airfoils/tests/

83
airfoil/data/as5046.dat Normal file
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AS5046 (16%)
1.0000 .00134
.99804 .00200
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1.0000 -.00134
http://amber.aae.uiuc.edu/~ashok/kr2/airfoils/tests/

83
airfoil/data/as5048.dat Normal file
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@ -0,0 +1,83 @@
AS5048 (18%)
1.0000 .00150
.99795 .00261
.99261 .00526
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1.0000 -.00149
http://amber.aae.uiuc.edu/~ashok/kr2/airfoils/tests/

80
airfoil/data/atr72sm.dat Normal file
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@ -0,0 +1,80 @@
Smoothed ATR airfoil coordinates obtained using AFSMO (Harry Morgan's NASA smoothing program)
1.00000 0.00000
0.96800 0.00510
0.94100 0.00977
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1.00000 0.00000

98
airfoil/data/august160.dat Normal file
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@ -0,0 +1,98 @@
AUGUST 160
1.00000 0.00000
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1.00000 0.00000

80
airfoil/data/avistar.dat Normal file
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AVISTAR
1.000000 0.001577
0.997540 0.002134
0.990700 0.003654
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1.000000 -0.001634

44
airfoil/data/b29root.dat Normal file
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B-29 ROOT AIRFOIL
19.0 21.0
0.0000000 0.0000000
0.0082707 0.0233088
0.0132000 0.0298517
0.0255597 0.0425630
0.0503554 0.0603942
0.0751941 0.0739301
0.1000570 0.0850687
0.1498328 0.1023515
0.1996558 0.1149395
0.2495240 0.1230325
0.2994312 0.1272298
0.3993490 0.1253360
0.4993711 0.1130538
0.5994664 0.0934796
0.6996058 0.0695104
0.7997553 0.0445423
0.8998927 0.0207728
0.9499514 0.0098870
1.0000000 0.0000000
0.0000000 0.0000000
0.0061140 -.0208973
0.0062188 -.0210669
0.0087532 -.0247377
0.0138088 -.0307807
0.0264052 -.0416431
0.0515127 -.0548774
0.0765762 -.0637165
0.1016176 -.0703581
0.1516652 -.0801452
0.2016828 -.0869356
0.2516733 -.0910290
0.3016387 -.0926252
0.4015163 -.0905235
0.5013438 -.0834273
0.6011363 -.0728351
0.7008976 -.0591463
0.8006328 -.0428603
0.9003380 -.0235778
0.9501740 -.0122883
1.0000000 0.0000000

44
airfoil/data/b29tip.dat Normal file
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@ -0,0 +1,44 @@
B-29 TIP AIRFOIL
19.0 21.0
0.0000000 0.0000000
0.0075149 0.0101442
0.0125046 0.0136584
0.0249843 0.0204940
0.0499554 0.0301654
0.0749328 0.0376370
0.0999142 0.0437086
0.1498843 0.0533519
0.1998618 0.0603954
0.2498462 0.0650390
0.2998375 0.0672827
0.3998371 0.0658704
0.4998552 0.0580585
0.5998839 0.0465468
0.6999180 0.0331352
0.7999519 0.0198236
0.8999808 0.0082119
0.9499917 0.0036560
1.0000000 -.0000000
0.0000000 0.0000000
0.0050092 -.0082226
0.0050680 -.0082620
0.0075716 -.0095547
0.0125762 -.0112403
0.0250839 -.0141042
0.0500918 -.0172321
0.0750953 -.0188601
0.1000975 -.0199881
0.1500994 -.0214442
0.2000997 -.0223003
0.2500985 -.0226564
0.3000964 -.0227126
0.4000917 -.0226249
0.5000867 -.0224372
0.6000798 -.0215496
0.7000698 -.0196620
0.8000548 -.0159745
0.9000326 -.0097872
0.9500182 -.0055435
1.0000000 -.0000000

100
airfoil/data/b540ols.dat Normal file
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@ -0,0 +1,100 @@
BELL 540 AIRFOIL (MODIFIED NACA 0012)
48. 48.
0. 0.
.00453 .01163
.00862 .01569
.01250 .01857
.01628 .02087
.02366 .02453
.03092 .02743
.03810 .02986
.04524 .03195
.05590 .03463
.06652 .03689
.08064 .03939
.09121 .04098
.10177 .04235
.11231 .04353
.12285 .04455
.13339 .04543
.15093 .04660
.17548 .04773
.20001 .04836
.21402 .04851
.22102 .04855
.22452 .04855
.23503 .04851
.25253 .04832
.28053 .04767
.30152 .04696
.32950 .04572
.35048 .04461
.38544 .04244
.42036 .04015
.45528 .03785
.49020 .03556
.52512 .03326
.56003 .03097
.59495 .02867
.62987 .02638
.66479 .02408
.69970 .02179
.73462 .01949
.76954 .01720
.80446 .01490
.83938 .01261
.87430 .01031
.90921 .00801
.94413 .00572
.97905 .00342
1.00000 .00205
0. 0.
.00453 -.01163
.00862 -.01569
.01250 -.01857
.01628 -.02087
.02366 -.02453
.03092 -.02743
.03810 -.02986
.04524 -.03195
.05590 -.03463
.06652 -.03689
.08064 -.03939
.09121 -.04098
.10177 -.04235
.11231 -.04353
.12285 -.04455
.13339 -.04543
.15093 -.04660
.17548 -.04773
.20001 -.04836
.21402 -.04851
.22102 -.04855
.22452 -.04855
.23503 -.04851
.25253 -.04832
.28053 -.04767
.30152 -.04696
.32950 -.04572
.35048 -.04461
.38544 -.04244
.42036 -.04015
.45528 -.03785
.49020 -.03556
.52512 -.03326
.56003 -.03097
.59495 -.02867
.62987 -.02638
.66479 -.02408
.69970 -.02179
.73462 -.01949
.76954 -.01720
.80446 -.01490
.83938 -.01261
.87430 -.01031
.90921 -.00801
.94413 -.00572
.97905 -.00342
1.00000 -.00205

126
airfoil/data/b707a.dat Normal file
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@ -0,0 +1,126 @@
BOEING 707 .08 SPAN AIRFOIL
61. 61.
0.0000000 0.0000000
0.0005000 0.0064638
0.0010000 0.0084488
0.0020000 0.0110085
0.0040000 0.0140317
0.0080000 0.0175265
0.0120000 0.0209530
0.0200000 0.0272234
0.0300000 0.0326742
0.0400000 0.0360978
0.0500000 0.0387719
0.0600000 0.0413505
0.0800000 0.0454360
0.1000000 0.0476525
0.1200000 0.0491397
0.1400000 0.0500832
0.1600000 0.0504598
0.1800000 0.0504723
0.2000000 0.0505076
0.2200000 0.0506790
0.2400000 0.0502123
0.2600000 0.0482429
0.2800000 0.0456843
0.3000000 0.0439763
0.3200000 0.0430062
0.3400000 0.0425267
0.3600000 0.0422943
0.3800000 0.0420659
0.4000000 0.0416033
0.4200000 0.0407363
0.4400000 0.0395394
0.4600000 0.0381409
0.4800000 0.0366673
0.5000000 0.0352476
0.5200000 0.0339760
0.5400000 0.0328278
0.5600000 0.0317559
0.5800000 0.0307107
0.6000000 0.0296456
0.6200000 0.0285267
0.6400000 0.0273739
0.6600000 0.0262196
0.6800000 0.0250949
0.7000000 0.0240321
0.7200000 0.0230489
0.7400000 0.0221102
0.7600000 0.0211718
0.7800000 0.0201870
0.8000000 0.0191108
0.8200000 0.0179036
0.8400000 0.0165478
0.8600000 0.0150329
0.8800000 0.0133449
0.9000000 0.0114733
0.9200000 0.0094145
0.9400000 0.0071976
0.9600000 0.0048649
0.9700000 0.0036652
0.9800000 0.0024506
0.9900000 0.0012275
1.0000000 0.0000000
0.0000000 0.0000000
0.0005000 -.0046938
0.0010000 -.0068122
0.0020000 -.0095513
0.0040000 -.0128330
0.0080000 -.0162748
0.0120000 -.0189872
0.0200000 -.0241108
0.0300000 -.0290301
0.0400000 -.0321990
0.0500000 -.0345765
0.0600000 -.0368498
0.0800000 -.0415383
0.1000000 -.0461846
0.1200000 -.0502606
0.1400000 -.0537201
0.1600000 -.0566756
0.1800000 -.0591680
0.2000000 -.0611521
0.2200000 -.0626515
0.2400000 -.0640784
0.2600000 -.0659499
0.2800000 -.0679186
0.3000000 -.0689475
0.3200000 -.0690421
0.3400000 -.0683785
0.3600000 -.0671287
0.3800000 -.0654627
0.4000000 -.0635503
0.4200000 -.0615419
0.4400000 -.0594897
0.4600000 -.0574125
0.4800000 -.0553319
0.5000000 -.0532648
0.5200000 -.0512286
0.5400000 -.0492102
0.5600000 -.0471911
0.5800000 -.0451534
0.6000000 -.0430761
0.6200000 -.0409454
0.6400000 -.0387685
0.6600000 -.0365568
0.6800000 -.0343263
0.7000000 -.0320878
0.7200000 -.0298565
0.7400000 -.0276400
0.7600000 -.0254497
0.7800000 -.0232958
0.8000000 -.0211866
0.8200000 -.0191282
0.8400000 -.0171026
0.8600000 -.0150853
0.8800000 -.0130551
0.9000000 -.0109869
0.9200000 -.0088630
0.9400000 -.0066907
0.9600000 -.0044805
0.9700000 -.0033653
0.9800000 -.0022462
0.9900000 -.0011243
1.0000000 0.0000000

36
airfoil/data/b707b.dat Normal file
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@ -0,0 +1,36 @@
BOEING 707 .19 SPAN AIRFOIL
16.0 16.0
0.000000 0.000000
0.004712 0.012211
0.007052 0.014766
0.012157 0.018787
0.024309 0.029274
0.049040 0.040657
0.073920 0.045745
0.098786 0.051431
0.148638 0.057708
0.198551 0.061386
0.248554 0.061266
0.298540 0.061846
0.398560 0.061006
0.498566 0.060766
0.598899 0.046634
1.000000 0.000000
0.000000 0.000000
0.005209 -0.008877
0.007681 -0.011919
0.012940 -0.014395
0.025467 -0.019799
0.050649 -0.027505
0.075755 -0.032012
0.100876 -0.037119
0.151044 -0.044235
0.201198 -0.050752
0.251319 -0.055869
0.301411 -0.059787
0.401417 -0.060027
0.501361 -0.057668
0.601185 -0.050212
1.000000 0.000000

38
airfoil/data/b707c.dat Normal file
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@ -0,0 +1,38 @@
BOEING 707 .40 SPAN AIRFOIL
17.0 17.0
0.0000 0.0000
0.0050 0.0149
0.0083 0.0165
0.0125 0.0206
0.0249 0.0256
0.0500 0.0330
0.0748 0.0396
0.1000 0.0446
0.1500 0.0545
0.2000 0.0578
0.2500 0.0628
0.3000 0.0661
0.4000 0.0661
0.5000 0.0611
0.6000 0.0512
0.7000 0.0413
1.0000 0.0000
0.0000 0.0000
0.0050 -0.0066
0.0083 -0.0074
0.0125 -0.0083
0.0249 -0.0091
0.0500 -0.0099
0.0748 -0.0124
0.1000 -0.0132
0.1500 -0.0165
0.2000 -0.0215
0.2500 -0.0248
0.3000 -0.0297
0.4000 -0.0297
0.5000 -0.0289
0.6000 -0.0264
0.7000 -0.0198
1.0000 0.0000

42
airfoil/data/b707d.dat Normal file
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@ -0,0 +1,42 @@
BOEING 707 .54 SPAN AIRFOIL
19.0 19.0
0.0000 0.0030
0.0050 0.0099
0.0074 0.0120
0.0126 0.0147
0.0250 0.0215
0.0500 0.0303
0.0753 0.0385
0.1000 0.0442
0.1500 0.0520
0.2000 0.0570
0.2500 0.0604
0.3000 0.0627
0.4000 0.0644
0.5000 0.0618
0.6000 0.0541
0.7000 0.0427
0.8000 0.0290
0.9000 0.0145
1.0000 0.0000
0.0000 0.0030
0.0050 -0.0046
0.0074 -0.0055
0.0126 -0.0065
0.0250 -0.0074
0.0500 -0.0090
0.0753 -0.0105
0.1000 -0.0118
0.1500 -0.0149
0.2000 -0.0177
0.2500 -0.0206
0.3000 -0.0227
0.4000 -0.0253
0.5000 -0.0250
0.6000 -0.0208
0.7000 -0.0156
0.8000 -0.0105
0.9000 -0.0051
1.0000 0.0000

126
airfoil/data/b707e.dat Normal file
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@ -0,0 +1,126 @@
BOEING 707 .99 SPAN AIRFOIL
61. 61.
0.0000000 0.0000000
0.0005000 0.0017762
0.0010000 0.0026712
0.0020000 0.0039826
0.0040000 0.0059651
0.0080000 0.0093775
0.0120000 0.0126235
0.0200000 0.0165502
0.0300000 0.0201909
0.0400000 0.0243663
0.0500000 0.0283931
0.0600000 0.0316763
0.0800000 0.0368998
0.1000000 0.0414470
0.1200000 0.0451368
0.1400000 0.0481068
0.1600000 0.0505979
0.1800000 0.0527383
0.2000000 0.0545539
0.2200000 0.0560793
0.2400000 0.0573984
0.2600000 0.0586036
0.2800000 0.0597119
0.3000000 0.0606677
0.3200000 0.0614255
0.3400000 0.0619894
0.3600000 0.0623757
0.3800000 0.0626003
0.4000000 0.0626795
0.4200000 0.0626219
0.4400000 0.0624084
0.4600000 0.0620130
0.4800000 0.0614093
0.5000000 0.0605710
0.5200000 0.0594744
0.5400000 0.0581322
0.5600000 0.0565812
0.5800000 0.0548590
0.6000000 0.0530032
0.6200000 0.0510426
0.6400000 0.0489701
0.6600000 0.0467699
0.6800000 0.0444259
0.7000000 0.0419222
0.7200000 0.0392571
0.7400000 0.0364864
0.7600000 0.0336812
0.7800000 0.0309114
0.8000000 0.0282480
0.8200000 0.0257350
0.8400000 0.0233138
0.8600000 0.0209021
0.8800000 0.0184162
0.9000000 0.0157729
0.9200000 0.0129100
0.9400000 0.0098530
0.9600000 0.0066502
0.9700000 0.0050090
0.9800000 0.0033495
0.9900000 0.0016777
1.0000000 -.0000000
0.0000000 0.0000000
0.0005000 -.0027391
0.0010000 -.0037318
0.0020000 -.0051549
0.0040000 -.0070820
0.0080000 -.0090008
0.0120000 -.0095219
0.0200000 -.0101876
0.0300000 -.0109695
0.0400000 -.0114902
0.0500000 -.0119380
0.0600000 -.0124717
0.0800000 -.0136395
0.1000000 -.0146775
0.1200000 -.0156764
0.1400000 -.0167361
0.1600000 -.0179398
0.1800000 -.0192399
0.2000000 -.0204561
0.2200000 -.0214592
0.2400000 -.0223472
0.2600000 -.0232692
0.2800000 -.0242397
0.3000000 -.0251365
0.3200000 -.0258576
0.3400000 -.0264065
0.3600000 -.0268131
0.3800000 -.0271073
0.4000000 -.0273189
0.4200000 -.0274668
0.4400000 -.0275250
0.4600000 -.0274563
0.4800000 -.0272236
0.5000000 -.0267894
0.5200000 -.0261207
0.5400000 -.0252416
0.5600000 -.0242160
0.5800000 -.0231082
0.6000000 -.0219837
0.6200000 -.0208931
0.6400000 -.0198331
0.6600000 -.0187862
0.6800000 -.0177353
0.7000000 -.0166627
0.7200000 -.0155566
0.7400000 -.0144264
0.7600000 -.0132873
0.7800000 -.0121541
0.8000000 -.0110418
0.8200000 -.0099608
0.8400000 -.0089020
0.8600000 -.0078516
0.8800000 -.0067959
0.9000000 -.0057209
0.9200000 -.0046164
0.9400000 -.0034854
0.9600000 -.0023346
0.9700000 -.0017538
0.9800000 -.0011706
0.9900000 -.0005857
1.0000000 0.0000000

50
airfoil/data/b737a.dat Normal file
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@ -0,0 +1,50 @@
BOEING 737 ROOT AIRFOIL
23. 23.
0.000000 0.017700
0.002300 0.030900
0.005000 0.037200
0.007600 0.041500
0.014300 0.049900
0.024900 0.058200
0.049500 0.073000
0.074000 0.081400
0.099000 0.086600
0.153000 0.090700
0.196100 0.090500
0.250400 0.088700
0.309400 0.085800
0.352000 0.083300
0.391900 0.080400
0.447700 0.075600
0.503400 0.069600
0.559300 0.062600
0.596500 0.057500
0.648800 0.049800
0.835100 0.022400
0.910900 0.013200
1.000000 0.000300
0.000000 0.017700
0.002200 0.003800
0.004900 -0.001800
0.007200 -0.005300
0.011900 -0.010600
0.024300 -0.020400
0.048600 -0.034200
0.071600 -0.045700
0.097900 -0.051600
0.148800 -0.060700
0.195300 -0.063200
0.250100 -0.063200
0.294500 -0.062600
0.357900 -0.061000
0.396500 -0.059500
0.454300 -0.056300
0.505000 -0.052700
0.555600 -0.048200
0.606300 -0.042700
0.648500 -0.037500
0.831700 -0.014900
0.941000 -0.005300
1.000000 -0.000300

50
airfoil/data/b737b.dat Normal file
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@ -0,0 +1,50 @@
BOEING 737 MIDSPAN AIRFOIL
23. 23.
0.000000 0.008800
0.002600 0.019800
0.004700 0.023600
0.007500 0.027500
0.012900 0.033200
0.022900 0.040800
0.053000 0.055200
0.073600 0.061300
0.099600 0.066600
0.151300 0.072800
0.208000 0.075600
0.250000 0.076100
0.297200 0.075600
0.360200 0.073400
0.407500 0.070500
0.454700 0.066700
0.510100 0.061400
0.552500 0.056700
0.600100 0.051200
0.700300 0.038800
0.826600 0.023300
0.902100 0.014200
1.000000 0.000400
0.000000 0.008800
0.002100 0.000400
0.005100 -0.003700
0.007800 -0.006200
0.013900 -0.010300
0.023000 -0.014700
0.050900 -0.024400
0.072500 -0.030100
0.096100 -0.035200
0.151300 -0.043200
0.208000 -0.047700
0.250000 -0.049300
0.309500 -0.050000
0.344900 -0.049800
0.398100 -0.048600
0.451200 -0.046300
0.506600 -0.042800
0.549000 -0.039700
0.596600 -0.035700
0.688900 -0.027500
0.850500 -0.013100
0.931300 -0.006000
1.000000 -0.000400

50
airfoil/data/b737c.dat Normal file
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@ -0,0 +1,50 @@
BOEING 737 MIDSPAN AIRFOIL
23. 23.
0.000000 0.000000
0.001900 0.005700
0.006000 0.010500
0.007800 0.012000
0.012900 0.015700
0.023700 0.021800
0.050500 0.032400
0.079400 0.040200
0.097500 0.044100
0.151100 0.052400
0.203600 0.057600
0.250000 0.060600
0.296400 0.062300
0.346800 0.062900
0.399000 0.062500
0.444700 0.060800
0.490400 0.059700
0.548600 0.052900
0.609100 0.047000
0.657100 0.042200
0.874100 0.018300
0.947000 0.007600
1.000000 0.000500
0.000000 0.000000
0.002200 -0.004000
0.004900 -0.005700
0.007000 -0.006600
0.012500 -0.007600
0.020900 -0.010100
0.055500 -0.014700
0.081600 -0.017400
0.107800 -0.020100
0.157100 -0.024700
0.203600 -0.028600
0.250000 -0.031900
0.296400 -0.034700
0.354900 -0.037000
0.399600 -0.037500
0.453200 -0.036600
0.491100 -0.035200
0.543400 -0.032800
0.626900 -0.028200
0.739600 -0.022000
0.783200 -0.019000
0.935400 -0.005600
1.000000 -0.000500

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